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Osama A. Kandil

  • Aeroelastic, CFD, and dynamic computation and optimization for buffet and flutter applicationAeroelastic, CFD, and dynamic computation and optimization for buffet and flutter application
  • Aeroelastic, CFD, and dynamics computation and optimization for buffet and flutter applicationsAeroelastic, CFD, and dynamics computation and optimization for buffet and flutter applications
  • Aerostructural vortical flow interactions with applications to F/A-18 and F-117 tail buffetAerostructural vortical flow interactions with applications to F/A-18 and F-117 tail buffet
  • Analysis and control of asymmetric vortex flows and supersonic vortex breakdownAnalysis and control of asymmetric vortex flows and supersonic vortex breakdown
  • Analysis and control of supersonic vortex breakdown flowsAnalysis and control of supersonic vortex breakdown flows
  • Analysis and mitigation of numerical dissipation in inviscid and viscid computation of vortex-dominated flowsAnalysis and mitigation of numerical dissipation in inviscid and viscid computation of vortex-dominated flows
  • Computation and validation of fluid/structure twin tail buffet responseComputation and validation of fluid/structure twin tail buffet response
  • Computation technique for compressible vortex flows using the integral equation solutionComputation technique for compressible vortex flows using the integral equation solution
  • Development of disturbances in swept wing flowsDevelopment of disturbances in swept wing flows
  • Effective control of computationally simulated wing rock in subsonic flowEffective control of computationally simulated wing rock in subsonic flow
  • Far-field turbulent vortex-wake/exhaust plume interaction for subsonic and HSCT airplanesFar-field turbulent vortex-wake/exhaust plume interaction for subsonic and HSCT airplanes
  • Navier-Stokes dynamics and aeroelastic computations for vortical flows, buffet and aeroelastic applicationsNavier-Stokes dynamics and aeroelastic computations for vortical flows, buffet and aeroelastic applications